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WO2016118980A4 - Aéronef - Google Patents

Aéronef Download PDF

Info

Publication number
WO2016118980A4
WO2016118980A4 PCT/ZA2016/000002 ZA2016000002W WO2016118980A4 WO 2016118980 A4 WO2016118980 A4 WO 2016118980A4 ZA 2016000002 W ZA2016000002 W ZA 2016000002W WO 2016118980 A4 WO2016118980 A4 WO 2016118980A4
Authority
WO
WIPO (PCT)
Prior art keywords
ball
collar
blade
aircraft according
socket joint
Prior art date
Application number
PCT/ZA2016/000002
Other languages
English (en)
Other versions
WO2016118980A2 (fr
WO2016118980A3 (fr
Inventor
Felix Errol GROENEWALD
Original Assignee
Groenewald Felix Errol
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Groenewald Felix Errol filed Critical Groenewald Felix Errol
Priority to US15/545,214 priority Critical patent/US20180002005A1/en
Publication of WO2016118980A2 publication Critical patent/WO2016118980A2/fr
Publication of WO2016118980A3 publication Critical patent/WO2016118980A3/fr
Publication of WO2016118980A4 publication Critical patent/WO2016118980A4/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/37—Rotors having articulated joints
    • B64C27/41—Rotors having articulated joints with flapping hinge or universal joint, common to the blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/52—Tilting of rotor bodily relative to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Transmission Devices (AREA)
  • Accessories For Mixers (AREA)

Abstract

Hélicoptère doté d'un rotor relié pivotant à un arbre par un joint universel ou une articulation sphérique. L'hélicoptère comprend : un fuselage; un mât de rotor qui est fixé à l'encontre une rotation relative par rapport au fuselage; au moins une pale; un moteur pour faire tourner la ou les pales; et un joint universel ou articulation sphérique. Le joint universel ou articulation sphérique: (i) est disposé entre la ou les pales et le mât de rotor, la ou les pales pouvant tourner par rapport au joint universel ou articulation sphérique; (ii) est disposé entre le moteur et le mât de rotor; et (iii) est fixé à l'encontre d'une rotation relative par rapport au mât de rotor, de telle sorte que, le pivotement du joint universel ou articulation sphérique provoque l'inclinaison de la ou des pales et du moteur.
PCT/ZA2016/000002 2015-01-21 2016-01-13 Aéronef WO2016118980A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US15/545,214 US20180002005A1 (en) 2015-01-21 2016-01-13 Aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ZA201500430 2015-01-21
ZA2015/00430 2015-01-21

Publications (3)

Publication Number Publication Date
WO2016118980A2 WO2016118980A2 (fr) 2016-07-28
WO2016118980A3 WO2016118980A3 (fr) 2016-11-24
WO2016118980A4 true WO2016118980A4 (fr) 2017-02-02

Family

ID=56417935

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ZA2016/000002 WO2016118980A2 (fr) 2015-01-21 2016-01-13 Aéronef

Country Status (2)

Country Link
US (1) US20180002005A1 (fr)
WO (1) WO2016118980A2 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11186363B2 (en) * 2015-10-21 2021-11-30 Sikorsky Aircraft Corporation Electric propulsion system for a rotary wing aircraft
US10752343B2 (en) 2016-10-18 2020-08-25 Sikorsky Aircraft Corporation Electric propulsion system for a rotary wing aircraft
US10618646B2 (en) * 2017-05-26 2020-04-14 Textron Innovations Inc. Rotor assembly having a ball joint for thrust vectoring capabilities
DE102017111911A1 (de) * 2017-05-31 2018-12-06 Dirk Brunner Antriebssystem für ein Fahrzeug
US10676182B2 (en) 2017-07-20 2020-06-09 Sikorsky Aircraft Corporation Tilting coaxial rotor for a rotary wing aircraft
US10974824B2 (en) 2017-07-20 2021-04-13 Sikorsky Aircraft Corporation Electric powered direct drive rotor motor
EP3508421A1 (fr) * 2018-01-09 2019-07-10 Microdrones GmbH Mécanisme d'entraînement d'hélicoptère et procédé de fonctionnement d'un mécanisme d'entraînement d'hélicoptère
US10946956B2 (en) * 2018-08-30 2021-03-16 Textron Innovations Inc. Unmanned aerial systems having out of phase gimballing axes
US12060148B2 (en) 2022-08-16 2024-08-13 Honeywell International Inc. Ground resonance detection and warning system and method

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3765794A (en) * 1972-02-18 1973-10-16 United Aircraft Corp Helicopter blade pitch lock
US4073600A (en) * 1976-06-14 1978-02-14 William Gallagher Damping mechanism for the rotor hub of a helicopter for ground resonance and waddle and its combination with the rotor
WO1984000339A1 (fr) * 1982-07-07 1984-02-02 Bernd Jung Helicoptere
US4702437A (en) * 1985-02-07 1987-10-27 Stearns Jr Hoyt A Electric air-driven helicopter
FR2725690B1 (fr) * 1994-10-13 1996-12-27 Eurocopter France Dispositif de commande de pas des pales d'un rotor de giravion
FR2761660B1 (fr) * 1997-04-08 1999-06-11 Onera (Off Nat Aerospatiale) Dispositif de commande individuelle des pales de rotor de voilures tournantes d'aeronefs avec plateaux cycliques multiples
FR2765550B1 (fr) * 1997-07-07 1999-10-01 Eurocopter France Dispositif de blocage en pas des pales d'un rotor principal de giravion
US6293492B1 (en) * 1998-09-02 2001-09-25 Engineering System Co., Ltd. Coaxial twin-rotor type helicopter
US6283757B1 (en) * 1998-10-09 2001-09-04 Simulation Entertainment Group, Inc. Full motion two seat interactive simulator
US7128293B2 (en) * 2003-12-04 2006-10-31 Reggald Emory Isley Helicopter
USD561084S1 (en) * 2006-01-19 2008-02-05 Silverlit Toys Manufactory, Ltd. Helicopter propeller
USD559764S1 (en) * 2006-01-19 2008-01-15 Silverlit Toys Manufactory, Ltd. Helicopter
US8002604B2 (en) * 2006-01-19 2011-08-23 Silverlit Limited Remote controlled toy helicopter
DE202007006976U1 (de) * 2007-05-15 2008-09-18 Jung, Nadine Hubschrauber
US8052500B2 (en) * 2008-11-25 2011-11-08 Silverlit Limited Helicopter with main and auxiliary rotors
NO330672B1 (no) * 2009-11-12 2011-06-06 Proxdynamics As Rotormekanisme for helikoptere
DE102010021024B4 (de) * 2010-05-19 2014-07-03 Eads Deutschland Gmbh Hauptrotorantrieb für Hubschrauber
US9440736B2 (en) * 2011-05-26 2016-09-13 Pete Bitar Special personal electric helicopter device with integral wind turbine recharging capability
WO2013056275A2 (fr) * 2011-10-12 2013-04-18 Groenewald Felix Errol Aéronef
US9169012B2 (en) * 2012-02-21 2015-10-27 Textron Innovations Inc. Coaxial counter-rotating rotor system
US9889929B2 (en) * 2013-03-14 2018-02-13 Bell Helicopter Textron Inc. Jam-tolerant linear control motor for hydraulic actuator valve
US9180964B2 (en) * 2013-03-15 2015-11-10 Bell Helicopter Textron Inc. Autorotative enhancement system
US9452830B2 (en) * 2014-01-13 2016-09-27 Sikorsky Aircraft Corporation Constant velocity drive for tilt rotor assembly
US10836478B2 (en) * 2015-08-24 2020-11-17 Sikorsky Aircraft Corporation Separation of collective and cyclic actuation

Also Published As

Publication number Publication date
WO2016118980A2 (fr) 2016-07-28
US20180002005A1 (en) 2018-01-04
WO2016118980A3 (fr) 2016-11-24

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